Download or read book Effect of Fin flare Combinations on the Aerodynamic Characteristics of a Body at Mach Numbers 1 61 and 2 20 written by Clyde Hayes and published by . This book was released on 1965 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Effect Opf Fin flare Combinations on the Aerodynamic Characteristics of a Body at Mach Numbers 1 61 and 2 20 written by Clyde Hayes and published by . This book was released on 1965 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Effects of Body and Fin Deflections on the Aerodynamic Characteristics in Pitch of a 0 065 scale Model of a Four stage Rocket Configuration at Mach Numbers of 1 41 and 1 82 written by Ross B. Robinson and published by . This book was released on 1959 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aerodynamic Characteristics of Several Cranked Leading edge Wing body Combinations at Mach Numbers from 0 4 to 2 94 written by Edward J. Hopkins and published by . This book was released on 1967 with total page 98 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Some Effects of Fin Plan Form on the Static Stability of Fin body Combinations at Mach Number 4 06 written by Edward F. Ulmann and published by . This book was released on 1952 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aerodynamic Characteristics at Mach Numbers from 1 50 to 4 63 of a Variable geometry Lifting Reentry Concept Employing Elevator and Body Base Flaps for Control written by Roger H. Fournier and published by . This book was released on 1967 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation of a lifting body configuration has been conducted in the Langley Unitary Plan wind tunnel through a Mach number range from 1.50 to 4.63 to determine the control effectiveness characteristics of body base flaps with and without anhedral tail elevator controls.
Download or read book A Note on the Drag Due to Lift of Delta Wings at Mach Numbers Up to 2 0 written by Robert S. Osborne and published by . This book was released on 1960 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Effects of Wing Planform on the Aerodynamic Characteristics of a Wing body tail Model at Mach Numbers 1 57 2 16 and 2 87 written by Royce L. McKinney and published by . This book was released on 1965 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Monthly Catalog of United States Government Publications written by United States. Superintendent of Documents and published by . This book was released on 1960 with total page 1812 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aerodynamic Characteristics Including Effect of Body Shape of a Mach 6 Aircraft Concept written by Gregory D. Riebe and published by . This book was released on 1983 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aerodynamic Characteristics of Nine Ogive Cylinder Flare Configurations at Mach Numbers of 1 1 to 4 5 written by James Robert Burt (Jr) and published by . This book was released on 1970 with total page 92 pages. Available in PDF, EPUB and Kindle. Book excerpt: A study of normal force, center of pressure, and axial force on nine ogive-cylinder-flare combinations is presented. The configurations were tested at Mach numbers of 1.1, 1.2, 1.3, 1.4, 1.5, 1.75, 2.5, 3.5, and 4.5. Angle of attack was varied from about -4.5 to 6.5 degrees. The effects of Mach number, flare length, and flare diameter on model normal force, center of pressure, and axial force are shown. (Author).
Download or read book A Transonic Investigation of Changing Indentation Design Mach Number on the Aerodynamic Characteristics of a 45 Degree Sweptback wing body Combination Designed for High Performance written by Donald L. Loving and published by . This book was released on 1961 with total page 92 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Effects of Wing Planform on the Aerodynamic Characteristics of a Wing body tail Model at Mach Numbers 3 96 and 4 63 written by Maurice O. Feryn and published by . This book was released on 1966 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book International Aerospace Abstracts written by and published by . This book was released on 1996 with total page 944 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Technical Publications Announcements with Indexes written by United States. National Aeronautics and Space Administration and published by . This book was released on 1962 with total page 1556 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book The Flow Past a Straight and a Swept wing body Combination and Their Equivalent Bodies of Revolution at Mach Numbers Near 1 0 written by W. F. Lindsey and published by . This book was released on 1954 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt: Abstract: The complete flow fields past a straight and a swept wing-body combination and their equivalent bodies of revolution at Mach numbers around 1.0 have been observed by means of motion-picture schlieren photography. The results of these observations indicate that the shock growth and positions on the wing-body combinations are closely reproduced in the flow past their respective equivalent bodies.
Download or read book Normal Force on Fin Flare Combinations at Mach Numbers from 1 1 to 4 5 written by James Robert Burt (Jr) and published by . This book was released on 1970 with total page 25 pages. Available in PDF, EPUB and Kindle. Book excerpt: A study of normal force on several slender fin-flare combinations is presented. The configurations were tested at Mach numbers of 1.1, 1.2, 1.3, 1.4, 1.5, 1.75, 2.5, 3.5, and 4.5. Angle of attack was carried from about -6.5 to 8.5 degrees. The effects due to varying Mach number on total model normal force and normal force due to the fins plus fin-body flow field interference are shown. Estimates of normal force of the fins plus fin-body interference are made from linearized small perturbation theory and compared to the test results. (Author).
